BR8807113A - DIFFUSER-INTENSIFIED AEROPOLY - Google Patents

DIFFUSER-INTENSIFIED AEROPOLY

Info

Publication number
BR8807113A
BR8807113A BR888807113A BR8807113A BR8807113A BR 8807113 A BR8807113 A BR 8807113A BR 888807113 A BR888807113 A BR 888807113A BR 8807113 A BR8807113 A BR 8807113A BR 8807113 A BR8807113 A BR 8807113A
Authority
BR
Brazil
Prior art keywords
aeropoly
intensified
diffuser
intensified aeropoly
Prior art date
Application number
BR888807113A
Other languages
Portuguese (pt)
Inventor
Mark T Willis
Original Assignee
Mark T Willis
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mark T Willis filed Critical Mark T Willis
Publication of BR8807113A publication Critical patent/BR8807113A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/28—Boundary layer controls at propeller or rotor blades
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Toys (AREA)
BR888807113A 1987-06-25 1988-06-23 DIFFUSER-INTENSIFIED AEROPOLY BR8807113A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US6622387A 1987-06-25 1987-06-25
PCT/US1988/002102 WO1988010210A1 (en) 1987-06-25 1988-06-23 Venturi enhanced airfoil

Publications (1)

Publication Number Publication Date
BR8807113A true BR8807113A (en) 1989-10-17

Family

ID=22068096

Family Applications (1)

Application Number Title Priority Date Filing Date
BR888807113A BR8807113A (en) 1987-06-25 1988-06-23 DIFFUSER-INTENSIFIED AEROPOLY

Country Status (6)

Country Link
EP (1) EP0319574A4 (en)
JP (1) JPH02501213A (en)
KR (1) KR890701417A (en)
AU (1) AU2325988A (en)
BR (1) BR8807113A (en)
WO (1) WO1988010210A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991009776A1 (en) * 1989-12-29 1991-07-11 Venturi Applications, Inc. Venturi-enhanced airfoil
EP2031243A1 (en) * 2007-08-31 2009-03-04 Lm Glasfiber A/S Means to maintain a flow attached to the exterior of a flow control member
GB0914838D0 (en) 2009-08-26 2009-09-30 Airbus Operations Ltd Aerofoil slot blowing
US9815545B1 (en) * 2017-02-28 2017-11-14 Steering Financial Ltd. Aerodynamic lifting system
JP2020032938A (en) * 2018-08-31 2020-03-05 幸福の科学 Flight body
FR3132543A1 (en) * 2022-02-07 2023-08-11 Safran Nacelles Aircraft comprising at least one fluidic propulsion device integrated into an element of the airframe and method of use

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2631794A (en) * 1947-07-22 1953-03-17 Douglas K Warner Airfoil nose flap arrangement
US2946540A (en) * 1948-09-13 1960-07-26 Sebac Nouvelle Sa Jet propelled aircraft
US2840323A (en) * 1956-05-17 1958-06-24 Bell Aircraft Corp Hinged airfoil with jet nozzle means for aircraft flight control
US2990138A (en) * 1956-10-02 1961-06-27 Power Jets Res & Dev Ltd Aircraft with turbine driven lifting fans
US3029045A (en) * 1957-08-28 1962-04-10 Bertin & Cie Ejector systems applicable to thrust generation or augmentation
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
US3063658A (en) * 1960-03-01 1962-11-13 Ii Roger W Griswold Supersonic airfoil with boundary layer control
FR1267920A (en) * 1960-06-15 1961-07-28 Snecma Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude
US3525474A (en) * 1968-12-09 1970-08-25 Us Air Force Jet pump or thrust augmentor
US3747874A (en) * 1971-08-25 1973-07-24 Rohr Corp Ejector nozzle having primary nozzles communicating with exhaust gases in plenum chamber
US3819134A (en) * 1972-11-30 1974-06-25 Rockwell International Corp Aircraft system lift ejector
US4442986A (en) * 1982-08-30 1984-04-17 The United States Of America As Represented By The Secretary Of The Navy Leading edge augmentor wing-in-ground effect vehicle

Also Published As

Publication number Publication date
KR890701417A (en) 1989-12-20
JPH02501213A (en) 1990-04-26
EP0319574A4 (en) 1990-09-05
AU2325988A (en) 1989-01-19
EP0319574A1 (en) 1989-06-14
WO1988010210A1 (en) 1988-12-29

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